CloudSat
![]() Artist's Concept of CloudSat | |
Mission type | Atmospheric research |
---|---|
Operator | NASA |
COSPAR ID | 2006-016A ![]() |
SATCAT no. | 29107 |
Website | CloudSat home page |
Mission duration | Planned: 22 months Final: 17 years, 11 months, 25 days |
Spacecraft properties | |
Bus | BCP-2000 |
Manufacturer | Ball Aerospace |
Launch mass | 700 kg (1,543 lb) |
Dimensions | 2.54 × 2.03 × 2.29 m (8.3 × 6.7 × 7.5 ft) (H × L × W) |
Start of mission | |
Launch date | April 28, 2006, 10:02:16 (2006-04-28UTC10:02:16) UTC |
Rocket | Delta II 7420-10C |
Launch site | Vandenberg, SLC-2W |
End of mission | |
Disposal | Passivated |
Deactivated | December 20, 2023, 11:10:30 UTC |
Last contact | 23 April 2024 (2024-04-24) (Decommissioned) |
Orbital parameters | |
Reference system | Geocentric |
Regime | LEO |
Semi-major axis | 7,080.59 km (4,399.67 mi) |
Eccentricity | 0.0000824 |
Perigee altitude | 709 km (441 mi) |
Apogee altitude | 710 km (440 mi) |
Inclination | 98.23 degrees |
Period | 98.83 minutes |
RAAN | 330.82 degrees |
Argument of perigee | 91.62 degrees |
Mean anomaly | 14.57 degrees |
Mean motion | 14.57 |
Epoch | 25 January 2015, 03:10:38 UTC[1] |
Revolution no. | 46,515 |
CloudSat is a Passivated NASA Earth observation satellite, which was launched on a Delta II rocket on April 28, 2006, and is awaiting disposal. It used radar to measure the altitude and properties of clouds, adding to the information on the relationship between clouds and climate to help resolve questions about global warming.[2]
It operated in daytime-only operations from 2011 to 2023 due to battery malfunction, requiring sunlight to power the radar. On December 20, 2023, the Cloud Profiling Radar was deactivated for the final time, ending the data collection portion of the mission.
The mission was selected under NASA's Earth System Science Pathfinder program in 1999. Ball Aerospace & Technologies Corp. in Boulder, Colorado, designed and built the spacecraft.
CloudSat's primary mission was scheduled to continue for 22 months to allow more than one seasonal cycle to be observed.
Instrument
![](http://upload.wikimedia.org/wikipedia/commons/thumb/d/d4/Delta_II_7420_on_Launch_Pad_SLC-2W.jpg/190px-Delta_II_7420_on_Launch_Pad_SLC-2W.jpg)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/2/2d/CloudSat_at_Vandenberg_AFB.jpg/190px-CloudSat_at_Vandenberg_AFB.jpg)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/1/11/Animation_of_CloudSat%27s_orbit.gif/300px-Animation_of_CloudSat%27s_orbit.gif)
The main instrument on CloudSat was the Cloud Profiling Radar (CPR), a 94-GHz nadir-looking radar that measures the power backscattered by clouds as a function of distance from the radar. The radar instrument was developed at NASA's Jet Propulsion Laboratory (JPL) in Pasadena, California, with hardware contributions from the Canadian Space Agency. The overall design of the CPR was simple, well understood, and had a strong heritage from the many cloud radars already in operation in ground-based and airborne applications. Most design parameters and subsystem configurations were nearly identical to those for the Airborne Cloud Radar, which has been flying on the NASA DC-8 aircraft since 1998.
The CPR capitalized on existing radar expertise and experience at JPL. Other radars already flown successfully or developed by JPL include the Seasat SAR, the Shuttle Imaging Radars (SIR-A, SIR-B, SIR-C), the Shuttle Radar Topography Mission (SRTM), Magellan Venus Radar Mapper, Cassini Radar (mapping Saturn's moon Titan), NSCAT, and SeaWinds.
Based on radar lifetime data, NASA expected the radar to operate for at least three years with a 99% probability.
CloudSat is managed by the Jet Propulsion Laboratory. Colorado State University provides scientific leadership and science data processing and distribution. The cost of this project was approximately $200 million.[3]
Impact on radio astronomy
Power levels of the CloudSat radar were such that the receiver electronics deployed on a typical radio telescope could be burned out if the telescope was pointing at the zenith during an overflight. Moreover, the typical receiver would probably saturate during an overflight (or near overflight) no matter where the radio telescope were pointed, and similarly strong signal levels would have been received if a telescope pointed at or near CloudSat whenever the satellite was above the horizon (which could be of order one hour per day at a typical location). The narrow-band, Doppler-shifted radar signal would probably have been detectable in even fairly short integrations no matter where a radio telescope were pointed, whenever CloudSat was above the horizon.[4][5][6]
See also
- A-train (satellite constellation)
- Earth Observing System
- List of spaceflights (2006)
References
- ^ "CLOUDSAT Satellite details 2006-016A NORAD 29107". N2YO. 25 January 2015. Retrieved 25 January 2015.
- ^ Stephens, Graeme L.; Vane, Deborah G.; Boain, Ronald J.; Mace, Gerald G.; Sassen, Kenneth; Wang, Zhien; Illingworth, Anthony J.; O'connor, Ewan J.; Rossow, William B.; Durden, Stephen L.; Miller, Steven D.; Austin, Richard T.; Benedetti, Angela; Mitrescu, Cristian (2002). "THE CLOUDSAT MISSION AND THE A-TRAIN: A New Dimension of Space-Based Observations of Clouds and Precipitation". Bulletin of the American Meteorological Society. 83 (12): 1771–1790. doi:10.1175/BAMS-83-12-1771. ISSN 0003-0007.
- ^ "CloudSat Press Kit" (PDF). NASA/JPL.
- ^ "Radio Astronomy and CloudSat". Scientific Committee on Frequency Allocations for Radio Astronomy and Space Science. Retrieved 13 March 2020.
- ^ "CLOUDSAT - consequences for Radio Astronomy". Institut de Radioastronomie Millimétrique. Retrieved 13 March 2020.
- ^ Liszt, Harvey (2020-01-08). "Radio Astronomy in a New Era of Satellite Radiocommunication". AAS 235. p. 27m08s. Archived from the original on 2021-12-21. Retrieved 13 March 2020.
External links
- Cloudsat home
- Cloudsat Data Processing Center
- CloudSat and the A Train
- CloudSat Mission Profile by NASA's Solar System Exploration
- Spacecraft seek climate clarity
- v
- t
- e
- Resurs-DK No.1
- KazSat-1
- Galaxy 16
- USA-187, USA-188, USA-189
- Progress M-57
- Kosmos 2421
- USA-184
- Hot Bird 8
- JCSAT-3A, Syracuse 3B
- Koreasat 5
- Shijian 8
- STS-115 (ITS P3/4)
- IGS-3A
- Chinasat-22A
- Kosmos 2423
- Soyuz TMA-9
- Hinode, HIT-SAT, SSSAT
- USA-190
- DirecTV-9S, Optus D1, LDREX
- MetOp-A
- Progress M-58
- Shijian 6C, Shijian 6D
- STEREO
- Sinosat-2
- XM-4
- Fengyun 2-05
- WildBlue 1, AMC-18
- STS-116 (ITS P5, SpaceHab LSM, ANDE-MAA, ANDE-FACL, RAFT1, MARScom, MEPSI-2)
- MEASAT-3
- USA-193
- TacSat-2, GeneSat
- Kiku 8
- SAR-Lupe 1
- Meridian 1
- Kosmos 2424, Kosmos 2425, Kosmos 2426
- CoRoT
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).